Movatterモバイル変換


[0]ホーム

URL:


EP1546642B1 - Method of isotropic deployment of the penetrators of a kinetic energy rod warhead with imploding charge - Google Patents

Method of isotropic deployment of the penetrators of a kinetic energy rod warhead with imploding charge
Download PDF

Info

Publication number
EP1546642B1
EP1546642B1EP03814579AEP03814579AEP1546642B1EP 1546642 B1EP1546642 B1EP 1546642B1EP 03814579 AEP03814579 AEP 03814579AEP 03814579 AEP03814579 AEP 03814579AEP 1546642 B1EP1546642 B1EP 1546642B1
Authority
EP
European Patent Office
Prior art keywords
warhead
penetrators
kinetic energy
core
explosive charge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP03814579A
Other languages
German (de)
French (fr)
Other versions
EP1546642A2 (en
EP1546642A4 (en
Inventor
Richard M. Lloyd
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Raytheon Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon CofiledCriticalRaytheon Co
Publication of EP1546642A2publicationCriticalpatent/EP1546642A2/en
Publication of EP1546642A4publicationCriticalpatent/EP1546642A4/en
Application grantedgrantedCritical
Publication of EP1546642B1publicationCriticalpatent/EP1546642B1/en
Anticipated expirationlegal-statusCritical
Expired - Lifetimelegal-statusCriticalCurrent

Links

Images

Classifications

Definitions

Landscapes

Description

    FIELD OF THE INVENTION
  • This invention relates to improvements in kinetic energy rod warheads.
  • RELATED APPLICATIONS
  • This application claims priority ofU.S. Provisional Application No. 60/406,828 filed August 29, 2002. This application is related toU.S. Application No. 09/938,022 filed August 23, 2001.
  • BACKGROUND OF THE INVENTION
  • Destroying missiles, aircraft, re-entry vehicles and other targets falls into three primary classifications: "hit-to-kill" vehicles, blast fragmentation warheads, and kinetic energy rod warheads.
  • "Hit-to-kill" vehicles are typically launched into a position proximate a re-entry vehicle or other target via a missile such as the Patriot, Trident or MX missile. The kill vehicle is navigable and designed to strike the re-entry vehicle to render it inoperable. Countermeasures, however, can be used to avoid the "hit-to-kill" vehicle. Moreover, biological warfare bomblets and chemical warfare submunition payloads are carried by some threats and one or more of these bomblets or chemical submunition payloads can survive and cause heavy casualties even if the "hit-to-kill" vehicle accurately strikes the target
  • Blast fragmentation type warheads are designed to be carried by existing missiles. Blast fragmentation type warheads, unlike "hit-to-kill" vehicles, are not navigable. Instead, when the missile carrier reaches a position close to an enemy missile or other target, a pre-made band of metal on the warhead is detonated and the pieces of metal are accelerated with high velocity and strike the target. The fragments, however, are not always effective at destroying the target and, again, biological bomblets and/or chemical submunition payloads survive and cause heavy casualties,
  • The textbook by the inventor hereof,R. Lloyd, "conventional Warhead Systems Physics and Engineering Design," Progress in Astronautics and Aeronautics (AIAA) Book Series, Vol. 179, ISBN 1-56347-255-4, 1998, incorporated herein by this reference, provides additional details concerning "hit-to-kill" vehicles and blast fragmentation type warheads. Chapter 5 of that textbook, proposes a kinetic energy rod warhead.
  • The two primary advantages of a kinetic energy rod warheads is that 1) it does not rely on precise navigation as is the case with "hit-to-kill" vehicles and 2) it provides better penetration then blast fragmentation type warheads.
  • The primary components associated with a conventional kinetic energy rod warhead is a hull, or a housing, a single projectile core or bay in the hull including a number of individual lengthy cylindrical projectiles, and an explosive charge in the center of the projectiles. When the explosive charge is detonated, the projectiles are deployed to impinge upon a re-entry vehicle, missile or other target hopefully destroying it and all the submunitions such as biological warfare bomblets or chemical warfare submunition payloads it carries.
  • A center core explosive charge in conjunction with an aimable rod warhead may result in a complex design, may occupy an inordinate amount of space, and add mass to the warhead.
  • Patent No.DE 19524 726 relates to a warhead casing to be forcibly broken by detonation. As disclosed therein, projectiles are directed in a transverse direction only.
  • SUMMARY OF THE INVENTION
  • This invention features a method of isotropically deploying the penetrators of a kinetic energy rod warhead, the method including the steps of: disposing a plurality of individual penetrators in the core of a hull surrounded by explosive charge section, and simultaneously detonating the charge sections to implode the core and isotropically deploy the penetrators in an isotropic pattern perpendicular with respect to a center axis.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Other objects, features and advantages will occur to those skilled in the art from the following description of a preferred embodiment and the accompanying drawings, in which:
    • Fig. 1 is schematic view showing the typical deployment of a "hit-to-kill" vehicle in accordance with the prior art;
    • Fig. 2 is schematic view showing the typical deployment of a prior art blast fragmentation type warhead;
    • Fig. 3 is schematic view showing the deployment of a theoretical kinetic energy rod warhead system;
    • Fig. 4A is a schematic cross-section view of one embodiment of the primary components of the method of isotropically firing the projectiles;
    • Fig. 4B is a schematic cross-sectional view showing the simultaneous detonation of explosive sections of the warhead shown inFig. 4A and the resulting shockwaves produced in accordance with the method of this invention;
    • Fig. 4C is a schematic cross-sectional view of the kinetic energy rod warhead shown inFig. 4B showing the circular isotropic pattern of rods produced in accordance with the method of this invention;
    • Fig. 5 is a flow chart showing the primary steps of the method of isotropically deploying the penetrators of the kinetic energy rod warhead of this invention.
    DISCLOSURE OF THE PREFERRED EMBODIMENT
  • Aside from the preferred embodiment or embodiments disclosed below, this invention is capable of other embodiments and of being practiced or being carried out in various ways. Thus, it is to be understood that the invention is not limited in its application to the details of construction and the arrangements of components set forth in the following description or illustrated in the drawings.
  • As discussed in the Background section above, "hit-to-kill" vehicles are typically launched into a position proximate are-entry vehicle 10,Fig. 1 or other target via amissile 12. "Hit-to-kill"vehicle 14 is navigable and designed to strikere-entry vehicle 10 to render it inoperable. Countermeasures, however, can be used to avoid the kill vehicle.Vector 16 shows killvehicle 14missing re-entry vehicle 10. Moreover, biological bomblets andchemical submunition payloads 18 are carried by some threats and one or more of these bomblets orchemical submunition payloads 18 can survive, as shown at 20, and cause heavy casualties even if killvehicle 14 does accurately striketarget 10.
  • Turning toFig. 2, blastfragmentation type warhead 32 is designed to be carried bymissile 30. When the missile reaches a position close to an enemy re-entry vehicle (RV), missile, orother target 36, a pre-made band of metal or fragments on the warhead is detonated and the pieces ofmetal 34strike target 36. The fragments, however, are not always effective at destroying the submunition target and, again, biological bomblets and/or chemical submunition payloads can survive and cause heavy casualties.
  • The textbook by the inventor hereof,R. Lloyd, "Conventional Warhead Systems Physics and Engineering Design," Progress in Astronautics and Aeronautics (AIAA) Book Series, Vol. 179, ISBN 1-56347-255-4, 1998 provides additional details concerning "hit-to-kill" vehicles and blast fragmentation type warheads, Chapter 5 of that textbook proposes a kinetic energy rod warhead.
  • One idea behind the subject invention is a warhead designed to deploy penetrators (rods or projectiles) in the trajectory path of a target by simultaneously detonating the explosive charge sections located about the hull of a kinetic energy warhead to create an implosion effect which acts on the core section of the warhead with penetrators therein. The resulting rebound energy created from the implosion effect on the core section ejects the penetrators in an isotropic pattern about the axis of the warhead.
  • In one embodiment, kinetic energy warhead with imploding charges for isotropicallyfiring projectiles 100,Fig. 4A includeshull 102 andcore 104 therein.Core 104 includes a plurality ofindividual penetrators 106, such as tungsten, titanium, or tantalum rods, and the like, which are typically individual lengthy cylindrical projectiles. Warhead 100 further includes explosive charge sections 108-122 surroundingcore 104. Detonators 124-138 (typically chip slapper type detonators) are used to initiate explosive charge sections 108-122, respectively; e.g.,detonator 124 initiatesexplosive charge section 108;detonator 126 initiatesexplosive charge section 110. Detonators 124-138 and explosive charge sections 108-122 are arranged to implode oncore 104 and isotropically deploy the plurality ofindividual penetrators 106. In one design, the simultaneous firing of detonators 124-138 initiates explosive charge sections 108-122, respectively, and produces an implosion effect, e.g. shock waves, oncore 104, as shown by arrows 140-154,Fig 4B. The imploding shock waves travel through the plurality ofpenetrators 106 withincore 104 and reflects back after intersecting withcenter 159 ofcore 104, thus generating rebound energy, as indicated byarrows 162, 164, and 166,Fig. 4C. The energy of the rebound is sufficient to eject plurality ofpenetrators 106 about thewarhead 100 in circularisotropic pattern 170 of penetrators aboutwarhead 100. Oncewarhead 100 is in position, a circularisotropic pattern 170 of penetrators is deployed which effectively destroys enemy missiles, aircraft, R.Vs, biological warfare bomblets and chemical bomblets, as well as any other enemy target. A unique feature of circularisotropic pattern 170 of penetrators is that missile orwarhead 100 appears larger than it actually is. Warhead 100 (e.g., an anti-ballistic missile) appears larger relative to the target because the projectiles (penetrators 106) are deployed in a 360 degree pattern (isotropic pattern 170) about the axis ofwarhead 100. In effect, the diameter ofwarhead 100 has increased by the dense radius of the spray pattern (isotropic pattern 170). These highly dense projectiles obtain high overall lethality whenwarhead 100 falls short of hitting the sweet spot of the payload.
  • As shown inFig. 4A, kineticenergy rod warhead 100 includes explosive charge sections 124-138 inhull 102 aboutcore 104 withpenetrators 106 therein. Shields, such asshield 180, separate explosive charge sections (e.g.,shield 180 separatesexplosive charge sections 108 and 110).Shield 180 may be made of a composite material, such as a steel core sandwiched between inner and outer lexan layers to prevent the detonation of one explosive charge section from detonating the other explosive charge sections.
  • In the prior art, isotropic deployment was possible but only with an explosive charge disposed in the center of a single set of projectiles. That design, in some cases, was somewhat complex, resulted in the explosive charge occupying an inordinate amount of space adding mass to the kinetic energy rod warhead and also resulted in less projectiles and hence less lethality. This prior art design in conjunction with an aimable kinetic energy device also requires added detonators and logic.
  • A unique feature ofwarhead 100 with explosive charge sections 124-138 located aboutcore 104 is that the need for a complex center core explosive charge is eliminated, hence simplifying the design ofwarhead 100. The overall mass ofwarhead 100 is thus reduced as is the amount of space required by the explosive charge sections, hence providing more space forprojectiles 106 which increases the lethality ofwarhead 100.
  • In some engagements that have a very small miss distance the predictor fuze may not know the exact location to deploy the rods (e.g., projectiles). In accordance with the subject invention,warhead 100 is designed to implode or pinch the rods (projectiles 106) away fromwarhead 100 without the need to add additional hardware to achieve such deployment.
  • The method of isotropically deploying the penetrators of a kinetic energy warhead of this invention includes the steps of: disposing a plurality ofindividual penetrators 106,Fig. 4A incore 104 ofhull 102 surrounded by explosive charge sections 108-122,step 300,Fig. 5; and detonating charge sections 108-122,Fig. 4A to implodecore 104 and isotropically deploypenetrators 106,Fig. 4C,step 302,Fig. 5. All the charge sections are detonated simultaneously, e.g., explosive charge sections 108-122,Fig. 4A to create acircular spray pattern 170,Fig. 4C.
  • Although specific features of the invention are shown in some drawings and not in others, this is for convenience only as each feature may be combined with any or all of the other features in accordance with the invention. The words "including", "comprising", "having", and "with" as used herein are to be interpreted broadly and comprehensively and are not limited to any physical interconnection. Moreover, any embodiments disclosed in the subject application are not to be taken as the only possible embodiments.
  • Other embodiments will occur to those skilled in the art and are within the following claim:

Claims (1)

  1. A method of isotropically deploying the penetrators of a kinetic energy rod warhead, the method comprising:
    disposing a plurality of individual penetrators (106) in the core (104) of a hull (102) surrounded by explosive charge sections (110, 112, 114, 116, 118, 120, 122); and
    simultaneously detonating the charge sections to implode (140, 142, 144, 146, 148, 150, 152, 154) the core and isotropically deploy the penetrators (106) in an isotropic pattern perpendicular with respect to a center axis (159) of the core (104).
EP03814579A2002-08-292003-08-06Method of isotropic deployment of the penetrators of a kinetic energy rod warhead with imploding chargeExpired - LifetimeEP1546642B1 (en)

Applications Claiming Priority (5)

Application NumberPriority DateFiling DateTitle
US40682802P2002-08-292002-08-29
US406828P2002-08-29
US3853192003-03-10
US10/385,319US7017496B2 (en)2002-08-292003-03-10Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators
PCT/US2003/024532WO2004061384A2 (en)2002-08-292003-08-06Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators

Publications (3)

Publication NumberPublication Date
EP1546642A2 EP1546642A2 (en)2005-06-29
EP1546642A4 EP1546642A4 (en)2009-06-03
EP1546642B1true EP1546642B1 (en)2012-11-21

Family

ID=32684757

Family Applications (1)

Application NumberTitlePriority DateFiling Date
EP03814579AExpired - LifetimeEP1546642B1 (en)2002-08-292003-08-06Method of isotropic deployment of the penetrators of a kinetic energy rod warhead with imploding charge

Country Status (7)

CountryLink
US (1)US7017496B2 (en)
EP (1)EP1546642B1 (en)
JP (1)JP4295224B2 (en)
AU (1)AU2003258085A1 (en)
CA (1)CA2496536C (en)
IL (1)IL167147A (en)
WO (1)WO2004061384A2 (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
USRE45899E1 (en)2000-02-232016-02-23Orbital Atk, Inc.Low temperature, extrudable, high density reactive materials
US7977420B2 (en)2000-02-232011-07-12Alliant Techsystems Inc.Reactive material compositions, shot shells including reactive materials, and a method of producing same
US20050199323A1 (en)2004-03-152005-09-15Nielson Daniel B.Reactive material enhanced munition compositions and projectiles containing same
US7614348B2 (en)*2006-08-292009-11-10Alliant Techsystems Inc.Weapons and weapon components incorporating reactive materials
US7624682B2 (en)2001-08-232009-12-01Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US7621222B2 (en)*2001-08-232009-11-24Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US8127686B2 (en)*2001-08-232012-03-06Raytheon CompanyKinetic energy rod warhead with aiming mechanism
US7624683B2 (en)2001-08-232009-12-01Raytheon CompanyKinetic energy rod warhead with projectile spacing
US20050109234A1 (en)*2001-08-232005-05-26Lloyd Richard M.Kinetic energy rod warhead with lower deployment angles
US20060283348A1 (en)*2001-08-232006-12-21Lloyd Richard MKinetic energy rod warhead with self-aligning penetrators
US7415917B2 (en)*2002-08-292008-08-26Raytheon CompanyFixed deployed net for hit-to-kill vehicle
US6931994B2 (en)*2002-08-292005-08-23Raytheon CompanyTandem warhead
WO2005099362A2 (en)2003-10-142005-10-27Raytheon CompanyMine counter measure system
FR2867469A1 (en)*2004-03-152005-09-16Alliant Techsystems IncReactive composition, useful in military and industrial explosives, comprises a metallic material defining a continuous phase and having an energetic material, which comprises oxidant and/or explosive of class 1.1
US20090320711A1 (en)*2004-11-292009-12-31Lloyd Richard MMunition
FR2887021B1 (en)*2005-06-142007-08-31Tda Armements Sas Soc Par Acti PENETRATING AID KIT COMPRISING A BOMB, IN PARTICULAR ANTI-INFRASTRUCTURE, PENETRANT PROJECTILE EQUIPPED WITH SUCH A KIT, AND METHOD OF PENETRATION IN A TARGET
WO2006136185A1 (en)*2005-06-212006-12-28Geke Technologie GmbhProjectile or warhead
EP1780494A3 (en)2005-10-042008-02-27Alliant Techsystems Inc.Reactive material enhanced projectiles and related methods
US7762196B1 (en)*2007-04-122010-07-27Lockheed Martin CorporationMunition containing sub-munitions that disperse in a circular delta grid impact pattern and method therefor
US9255774B2 (en)2008-06-302016-02-09Battelle Memorial InstituteControlled fragmentation of a warhead shell
FR2950137B1 (en)*2009-09-112016-08-19Tda Armements Sas MISSILE CHARGE WITH RODS DEPLOYABLE BY ENERGY RESTITUTION AND METHOD OF ACTIVATING SUCH CHARGE
US20120186482A1 (en)*2010-04-022012-07-26Lloyd Richard MKinetic energy rod warhead with blast fragmentation
US8418623B2 (en)2010-04-022013-04-16Raytheon CompanyMulti-point time spacing kinetic energy rod warhead and system
CN111412792B (en)*2020-04-222024-11-26贵州省材料产业技术研究院 A piston-type dispersion mechanism
IL284594A (en)*2021-07-042023-02-01Cohen DavidInterceptor
CN114166075A (en)*2021-10-082022-03-11南京理工大学Expansion type warhead device capable of controlling fragment direction of warhead

Family Cites Families (99)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US1198035A (en)*1915-12-141916-09-12William Caldwell HuntingtonProjectile.
US1229421A (en)*1917-03-211917-06-12George E GrovesProjectile.
US1235076A (en)*1917-06-021917-07-31Edwin S StantonTorpedo-guard.
US1244046A (en)1917-07-201917-10-23Robert FfrenchProjectile.
US1300333A (en)1918-04-081919-04-15Leroy A BerryExplosive shell.
US1305967A (en)*1918-05-221919-06-03Edward A HawksExplosive shell.
US2308683A (en)*1938-12-271943-01-19John D ForbesChain shot
US2322624A (en)*1939-10-061943-06-22John D ForbesChain shot
US2296980A (en)*1940-10-171942-09-29Oric Scott HoberShell
GB550001A (en)1941-07-161942-12-17Lewis MotleyImprovements in or relating to ordnance projectiles
US2337765A (en)*1942-12-311943-12-28Nahirney JohnBomb
US4147108A (en)*1955-03-171979-04-03Aai CorporationWarhead
US2925965A (en)*1956-03-071960-02-23Collins Radio CoGuided missile ordnance system
US2988994A (en)1957-02-211961-06-20Jr Carl W FleischerShaped charge with cylindrical liner
US3877376A (en)*1960-07-271975-04-15Us NavyDirected warhead
US3332348A (en)*1965-01-221967-07-25Jack A MyersNon-lethal method and means for delivering incapacitating agents
US5182418A (en)*1965-06-211993-01-26The United States Of America As Represented By The Secretary Of The NavyAimable warhead
US3903804A (en)*1965-09-271975-09-09Us NavyRocket-propelled cluster weapon
US3949674A (en)*1965-10-221976-04-13The United States Of America As Represented By The Secretary Of The NavyOperation of fragment core warhead
US3757694A (en)*1965-10-221973-09-11Us NavyFragment core warhead
US3796159A (en)*1966-02-011974-03-12Us NavyExplosive fisheye lens warhead
US3861314A (en)*1966-12-301975-01-21Aai CorpConcave-compound pointed finned projectile
US3851590A (en)*1966-12-301974-12-03Aai CorpMultiple hardness pointed finned projectile
US3941059A (en)1967-01-181976-03-02The United States Of America As Represented By The Secretary Of The ArmyFlechette
US3954060A (en)1967-08-241976-05-04The United States Of America As Represented By The Secretary Of The ArmyProjectile
US4430941A (en)1968-05-271984-02-14Fmc CorporationProjectile with supported missiles
US3915092A (en)*1968-06-041975-10-28Aai CorpUnderwater projectile
US3846878A (en)*1968-06-041974-11-12Aai CorpMethod of making an underwater projectile
US4106410A (en)*1968-08-261978-08-15Martin Marietta CorporationLayered fragmentation device
US3565009A (en)1969-03-191971-02-23Us NavyAimed quadrant warhead
US3665009A (en)*1969-08-181972-05-23Du Pont1-carbamolypyrazole-4-sulfonamides
US3656433A (en)1969-10-131972-04-18Us ArmyMethod for reducing shot dispersion
US4745864A (en)1970-12-211988-05-24Ltv Aerospace & Defense CompanyExplosive fragmentation structure
US4026213A (en)*1971-06-171977-05-31The United States Of America As Represented By The Secretary Of The NavySelectively aimable warhead
US4211169A (en)1971-07-301980-07-08The United States Of America As Represented By The Secretary Of The ArmySub projectile or flechette launch system
US4210082A (en)1971-07-301980-07-01The United States Of America As Represented By The Secretary Of The ArmySub projectile or flechette launch system
US3771455A (en)1972-06-061973-11-13Us ArmyFlechette weapon system
US3797359A (en)1972-08-141974-03-19Me AssMulti-flechette weapon
US3818833A (en)1972-08-181974-06-25Fmc CorpIndependent multiple head forward firing system
DE2308912C3 (en)1973-02-231981-01-08Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Electric ignition system for the explosive charge of a warhead or the like
US3902424A (en)*1973-12-071975-09-02Us ArmyProjectile
US4089267A (en)1976-09-291978-05-16The United States Of America As Represented By The Secretary Of The ArmyHigh fragmentation munition
US4036140A (en)1976-11-021977-07-19The United States Of America As Represented Bythe Secretary Of The ArmyAmmunition
US4231293A (en)*1977-10-261980-11-04The United States Of America As Represented By The Secretary Of The Air ForceSubmissile disposal system
DE2835817C2 (en)*1978-08-161985-03-21Rheinmetall GmbH, 4000 Düsseldorf In a cargo floor to several active bodies arranged one behind the other so that they can be ejected, with several daughter floors arranged in radially directed launching tubes
US4172407A (en)*1978-08-251979-10-30General Dynamics CorporationSubmunition dispenser system
DE3016861C2 (en)*1980-05-021984-07-12Messerschmitt-Bölkow-Blohm GmbH, 8000 München Warhead with a shell for fragmentation
US4376901A (en)1981-06-081983-03-15The United States Of America As Represented By The United States Department Of EnergyMagnetocumulative generator
FR2678723B1 (en)1981-06-261993-11-12Etat Francais EXPLOSIVE PROJECTILE, ESPECIALLY ANTI-AIR, INCLUDING A LOAD WITH ROTARY DIRECTIONAL EFFECT.
US4455943A (en)*1981-08-211984-06-26The Boeing CompanyMissile deployment apparatus
DE3306659A1 (en)*1983-02-251984-08-30Rheinmetall GmbH, 4000 Düsseldorf ACTION UNIT
DE3327043A1 (en)1983-07-271985-02-07Technisch-Mathematische Studiengesellschaft mbH, 5300 BonnDevice for scattering electromagnetic decoy material, particularly from a rocket
US4655139A (en)1984-09-281987-04-07The Boeing CompanySelectable deployment mode fragment warhead
US4848239A (en)1984-09-281989-07-18The Boeing CompanyAntiballistic missile fuze
US4658727A (en)1984-09-281987-04-21The Boeing CompanySelectable initiation-point fragment warhead
US4638737A (en)1985-06-281987-01-27The United States Of America As Represented By The Secretary Of The ArmyMulti-warhead, anti-armor missile
US4676167A (en)*1986-01-311987-06-30Goodyear Aerospace CorporationSpin dispensing method and apparatus
CA1266202A (en)1986-06-051990-02-27William J. RobertsonMultiple flechette warhead
FR2606135B1 (en)*1986-10-311990-07-27Thomson Brandt Armements PROJECTILE COMPRISING SUB-PROJECTILES WITH CONTROLLED DIRECTIONAL WIDTH
GB2226624B (en)*1987-12-121991-07-03Thorn Emi Electronics LtdProjectile
US4922826A (en)1988-03-021990-05-08Diehl Gmbh & Co.Active component of submunition, as well as flechette warhead and flechettes therefor
US4996923A (en)1988-04-071991-03-05Olin CorporationMatrix-supported flechette load and method and apparatus for manufacturing the load
JPH01296100A (en)1988-05-191989-11-29Mitsubishi Electric CorpDetonating assembly for warhead
DE3830527A1 (en)1988-09-081990-03-22Diehl Gmbh & Co PROJECT-FORMING INSERT FOR HOLLOW LOADS AND METHOD FOR PRODUCING THE INSERT
DE3843796A1 (en)*1988-12-241990-07-05Rheinmetall Gmbh FLOOR WITH SIDE CONTROL
DE3932952A1 (en)1989-10-031991-04-11Rheinmetall Gmbh BULLET STOCK
DE3934042A1 (en)1989-10-121991-04-25Diehl Gmbh & CoWarhead with sub-munitions - has explosive charges to break up housing and to scatter sub-munitions
GB9014653D0 (en)*1989-10-181997-11-05Messerschmitt Boelkow BlohmAuswerfen und verteilen von submunition
US5313890A (en)*1991-04-291994-05-24Hughes Missile Systems CompanyFragmentation warhead device
USH1048H (en)1991-08-051992-05-05The United States Of America As Represented By The Secretary Of The NavyComposite fragmenting rod for a warhead case
USH1047H (en)1991-08-051992-05-05The United States Of America As Represented By The Secretary Of The NavyFragmenting notched warhead rod
DE4139372C1 (en)1991-11-291995-03-02Deutsche AerospaceFragmentation warhead
US5223667A (en)*1992-01-211993-06-29Bei Electronics, Inc.Plural piece flechettes affording enhanced penetration
US5229542A (en)1992-03-271993-07-20The United States Of America As Represented By The United States Department Of EnergySelectable fragmentation warhead
US5370053A (en)1993-01-151994-12-06Magnavox Electronic Systems CompanySlapper detonator
IL108095A (en)1993-12-201999-05-09Israel StateChemical system for accelerating projectiles to hypervelocity
DE4409424C1 (en)*1994-03-181995-08-10Daimler Benz Aerospace AgCatchment device for flying objects
FR2721701B1 (en)*1994-06-281996-08-14Giat Ind Sa Tail for a projectile, in particular for a sub-calibrated supersonic projectile.
DE19524726B4 (en)1994-08-102006-05-24Rheinmetall W & M Gmbh warhead
US5524524A (en)*1994-10-241996-06-11Tracor Aerospace, Inc.Integrated spacing and orientation control system
IL115749A (en)1994-10-272000-02-29Thomson CsfMissile launching and orientating system
US5535679A (en)*1994-12-201996-07-16Loral Vought Systems CorporationLow velocity radial deployment with predetermined pattern
DE4445991A1 (en)1994-12-221996-06-27Rheinmetall Ind Gmbh Ignition system for propellant charges and method for producing such ignition systems
US5691502A (en)1995-06-051997-11-25Lockheed Martin Vought Systems Corp.Low velocity radial deployment with predeterminded pattern
JP3065669B2 (en)*1995-06-072000-07-17レイセオン・カンパニー Aerodynamically stable bullet system for use against underwater targets.
US5542354A (en)1995-07-201996-08-06Olin CorporationSegmenting warhead projectile
SE508652C2 (en)1995-10-051998-10-26Bofors Ab Ways to distinguish false zone tube indications from indications of real targets as well as explosives filled with zone tube projectile
EP0873494A4 (en)1996-01-252000-12-27Remington Arms Co IncLead-free frangible projectile
DE19619341C2 (en)*1996-05-141999-11-11Rheinmetall W & M Gmbh Sub-caliber balancing projectile and method for its production
USD380784S (en)*1996-05-291997-07-08Great Lakes Dart Distributors, Inc.Dart
US6279482B1 (en)*1996-07-252001-08-28Trw Inc.Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket
US5796031A (en)1997-02-101998-08-18Primex Technologies, Inc.Foward fin flechette
US6279478B1 (en)*1998-03-272001-08-28Hayden N. RingerImaging-infrared skewed-cone fuze
US6186070B1 (en)1998-11-272001-02-13The United States Of America As Represented By The Secretary Of The ArmyCombined effects warheads
US6276277B1 (en)*1999-04-222001-08-21Lockheed Martin CorporationRocket-boosted guided hard target penetrator
SE518526C2 (en)*2000-07-032002-10-22Bofors Weapon Sys Ab Ammunition unit charging unit
US6598534B2 (en)*2001-06-042003-07-29Raytheon CompanyWarhead with aligned projectiles
US6666145B1 (en)*2001-11-162003-12-23Textron Systems CorporationSelf extracting submunition
US6622632B1 (en)2002-03-012003-09-23The United States Of America As Represented By The Secretary Of The NavyPolar ejection angle control for fragmenting warheads

Also Published As

Publication numberPublication date
EP1546642A2 (en)2005-06-29
EP1546642A4 (en)2009-06-03
JP4295224B2 (en)2009-07-15
US7017496B2 (en)2006-03-28
CA2496536A1 (en)2004-07-22
CA2496536C (en)2008-07-15
US20040129162A1 (en)2004-07-08
WO2004061384A3 (en)2004-11-04
AU2003258085A1 (en)2004-07-29
WO2004061384A2 (en)2004-07-22
JP2006508323A (en)2006-03-09
AU2003258085A8 (en)2004-07-29
IL167147A (en)2010-11-30

Similar Documents

PublicationPublication DateTitle
EP1546642B1 (en)Method of isotropic deployment of the penetrators of a kinetic energy rod warhead with imploding charge
US6598534B2 (en)Warhead with aligned projectiles
US7143698B2 (en)Tandem warhead
EP1583933B1 (en)Fixed deployed net for hit-to-kill vehicle
US6910423B2 (en)Kinetic energy rod warhead with lower deployment angles
US20040055498A1 (en)Kinetic energy rod warhead deployment system
US7040235B1 (en)Kinetic energy rod warhead with isotropic firing of the projectiles
JP2008512642A (en) Kinetic energy rod warhead with narrow open angle
US8127686B2 (en)Kinetic energy rod warhead with aiming mechanism
US20060021538A1 (en)Kinetic energy rod warhead deployment system

Legal Events

DateCodeTitleDescription
PUAIPublic reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text:ORIGINAL CODE: 0009012

17PRequest for examination filed

Effective date:20050224

AKDesignated contracting states

Kind code of ref document:A2

Designated state(s):AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AXRequest for extension of the european patent

Extension state:AL LT LV MK

DAXRequest for extension of the european patent (deleted)
A4Supplementary search report drawn up and despatched

Effective date:20090508

17QFirst examination report despatched

Effective date:20091207

REGReference to a national code

Ref country code:DE

Ref legal event code:R079

Ref document number:60342671

Country of ref document:DE

Free format text:PREVIOUS MAIN CLASS: F42B0012600000

Ipc:F41H0011040000

GRAJInformation related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text:ORIGINAL CODE: EPIDOSDIGR1

GRAPDespatch of communication of intention to grant a patent

Free format text:ORIGINAL CODE: EPIDOSNIGR1

GRAPDespatch of communication of intention to grant a patent

Free format text:ORIGINAL CODE: EPIDOSNIGR1

RIC1Information provided on ipc code assigned before grant

Ipc:F42B 12/22 20060101ALI20120531BHEP

Ipc:F42B 12/64 20060101ALI20120531BHEP

Ipc:F42B 12/60 20060101ALI20120531BHEP

Ipc:F42B 12/58 20060101ALI20120531BHEP

Ipc:F41H 13/00 20060101ALI20120531BHEP

Ipc:F42C 19/095 20060101ALI20120531BHEP

Ipc:F41H 11/04 20060101AFI20120531BHEP

Ipc:F42B 12/32 20060101ALI20120531BHEP

Ipc:F42B 12/20 20060101ALI20120531BHEP

GRASGrant fee paid

Free format text:ORIGINAL CODE: EPIDOSNIGR3

GRAA(expected) grant

Free format text:ORIGINAL CODE: 0009210

AKDesignated contracting states

Kind code of ref document:B1

Designated state(s):AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REGReference to a national code

Ref country code:GB

Ref legal event code:FG4D

REGReference to a national code

Ref country code:CH

Ref legal event code:EP

REGReference to a national code

Ref country code:AT

Ref legal event code:REF

Ref document number:585300

Country of ref document:AT

Kind code of ref document:T

Effective date:20121215

REGReference to a national code

Ref country code:IE

Ref legal event code:FG4D

REGReference to a national code

Ref country code:DE

Ref legal event code:R096

Ref document number:60342671

Country of ref document:DE

Effective date:20130117

REGReference to a national code

Ref country code:NL

Ref legal event code:VDEP

Effective date:20121121

REGReference to a national code

Ref country code:AT

Ref legal event code:MK05

Ref document number:585300

Country of ref document:AT

Kind code of ref document:T

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:ES

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20130304

Ref country code:FI

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:SE

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:GR

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20130222

Ref country code:PT

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20130321

Ref country code:BE

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:SI

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:AT

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:CZ

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:SK

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:BG

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20130221

Ref country code:DK

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:EE

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:RO

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:NL

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PLBENo opposition filed within time limit

Free format text:ORIGINAL CODE: 0009261

STAAInformation on the status of an ep patent application or granted ep patent

Free format text:STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26NNo opposition filed

Effective date:20130822

REGReference to a national code

Ref country code:DE

Ref legal event code:R097

Ref document number:60342671

Country of ref document:DE

Effective date:20130822

REGReference to a national code

Ref country code:CH

Ref legal event code:PL

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:CH

Free format text:LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date:20130831

Ref country code:LI

Free format text:LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date:20130831

Ref country code:MC

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

REGReference to a national code

Ref country code:IE

Ref legal event code:MM4A

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:IE

Free format text:LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date:20130806

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:TR

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

Ref country code:CY

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date:20121121

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:LU

Free format text:LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date:20130806

Ref country code:HU

Free format text:LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date:20030806

REGReference to a national code

Ref country code:FR

Ref legal event code:PLFP

Year of fee payment:14

REGReference to a national code

Ref country code:FR

Ref legal event code:PLFP

Year of fee payment:15

REGReference to a national code

Ref country code:FR

Ref legal event code:PLFP

Year of fee payment:16

PGFPAnnual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code:IT

Payment date:20220720

Year of fee payment:20

Ref country code:GB

Payment date:20220721

Year of fee payment:20

Ref country code:DE

Payment date:20220616

Year of fee payment:20

PGFPAnnual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code:FR

Payment date:20220721

Year of fee payment:20

REGReference to a national code

Ref country code:DE

Ref legal event code:R071

Ref document number:60342671

Country of ref document:DE

REGReference to a national code

Ref country code:GB

Ref legal event code:PE20

Expiry date:20230805

PG25Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code:GB

Free format text:LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date:20230805


[8]ページ先頭

©2009-2025 Movatter.jp